A bifurcated inlet scoop frame for a gas turbine engine and method of using such frame for a gas turbine engine are disclosed. The bifurcated inlet scoop frame having a nose, a first side panel, and a second side panel. The first side panel and the nose defining a first inlet port. The second side panel and the nose defining a second inlet port. The method including the steps of providing a bifurcated inlet scoop frame, splitting the fan air flow, and receiving fan air through the bifurcated inlet scoop frame.
Bifurcated inlet scoop for gas turbine engine
2019-08-20
Patent
Electronic Resource
English
GAS TURBINE ENGINE HAVING A BIFURCATED AIR INLET HOUSING
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